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. CL-600-2D15 (Regional Jet Series 705): 75 passengers configuration (plus 5 crewmembers)
The aircraft is certified for a maximum altitude of 41,000 feet and a maximum design airspeed of Mach 0.85. The Mach number must be decreased to Mach 0.84 above 34,000 feet. The airframe is a monocoque design, using lightweight aluminum alloys, alloy steels, stainless steels, titanium and composite materials. It has a low, high swept wing, T-tail with trimmable horizontal stabilizer and tricycle landing gear.
1.
EASA/JAA Type Design Definition
Reference CRI A-900-06 JAA/EASA Build Standard Definition, RAZ-BA690-120.
2.
Engines
Two General Electric CF34-8C5 or optional CF34-8C5A1 Turbofan Engines, with reverse thrust capability, are rear fuselage mounted on pylons; JAA Executive Board recommendation letter 04/12/91/10/02-L237 dated 20 September 2002. Appropriate National Authority Type Certificate or FAA Engine Type Certificate No. E00063EN Revision 2 or later, and associated Type Certificate Data Sheet.
Engine Limits:
Refer to the Airplane Flight Manual (CSP C-012).
3. Fuel
Type SPECIFICATION
Canada USA UK
Kerosene JET A, A-1 JP8 CAN 2 – 3.23 3-GP-23 ASTM D1655 MIL-DTL-83133 Def Stan 91-91 Def Stan 91-87
High Flash JP5 3-GP-24 MIL-DTL-5624 Def Stan 91-86
Note: Fuel additives -See AFM as listed in Approved Publications
For additional approved fuel grades see AFM.
For fuel temperature limitations see applicable AFM.
Fuel Capacity:
Load Weight
Usable U.S. Gal. Litres lb. kg
2 main tanks (each) 1,110 4,202 7,492 3,398
1 Center Tank 683 2,585 4,610 2,091
Total 2,903 10,989 19,595 8,888
Load Weight
U.S. Gal. Litres lb. kg
Unusable 23.1 87.4 155.9 70.7
Undrainable 2.0 7.6 13.5 6.1
4.
Oil Oil: Engine, APU: MIL-L-7808 (Type I) or MIL-L-23699 (Type II) or Castrol 4000 Mixing of different types of oils is prohibited Oil Capacity:
5.
Air Speeds:
6.
Centre of Gravity Range See AFM, CSP C-012. Datum: FS 0.0 located at 365.76cm (144.00 inches) forward of the aircraft nose Mean Aerodynamic Cord (MAC):
Load Weight
Usable U.S. Quart Litres lb. kg.
2 Engines (each) 7.2 6.8 14.6 6.6
Total 14.4 13.6 29.2 13.2
Airspeed Limits (IAS) Knots Mach VMO and MMO (Maximum Operating) Below 8000 feet 330* * *See AFM (CSP B-012) for variations of VMO and MMO at or above 8000 ft
VFE (Flaps extended) 1° 8° 20° 30° 45° 230 230 220 185 170
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本文链接地址：European Aviation Safety Agency TYPE-CERTIFICATE DATA SHEET CL-600(12)
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